Advanced aircraft power system and its control system was introduced and fault tolerant design of data bus was discussed.
介绍了先进飞机供电系统及其控制系统的组成，并对数据通信总线的容错设计进行论述。
This paper presents a fault-tolerant software design method and its application to the micro-controller system (MCS-51) of a type of Pilotless aircraft.
本文介绍了某型无人驾驶飞机系列MCS - 51单片机控制系统的软件容错设计方法与实现。
The purpose of this paper is to apply fault tolerant control theories to the design of electro hydraulic servo system in order to raise its reliability.
本文目的旨在把当今前沿的容错控制理论应用到电液伺服系统设计中去，以提高其可靠性。
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